Puck (moon of Uranus)

Document v1 · published by Koskamo · updated 2026-10-05

Puck is a natural satellite of Uranus in the NASA/JPL Solar System Dynamics planetary satellite tables.

Planet: Uranus
Satellite: Puck
Satellite code: 715
Physical parameters: not listed in the NASA/JPL planetary satellite physical parameters table
Ephemeris: URA182
Reference frame: equatorial
Epoch (TDB): 2000-01-01.5
Semi-major axis a: 86004. km
Eccentricity e: 0.000
Argument of periapsis ω: 0.0 deg
Mean anomaly M: 50.1 deg
Inclination i: 0.3 deg
Longitude of ascending node: 216.1 deg
Sidereal period P: 0.761833 days
Argument of periapsis precession period: 2.226 yr
Longitude of ascending node precession period: 4.454 yr
Mean elements reference: 45
Second solution ephemeris: URA184
Second solution reference frame: Laplace
Second solution epoch (TDB): 2025-01-01.0
Second solution semi-major axis a: 86007. km
Second solution eccentricity e: 0.009
Second solution argument of periapsis ω: 337.0 deg
Second solution mean anomaly M: 264.1 deg
Second solution inclination i: 1.1 deg
Second solution longitude of ascending node: 111.2 deg
Second solution sidereal period P: 0.7618 days
Second solution argument of periapsis precession period: 1.9 yr
Second solution longitude of ascending node precession period: 3.9 yr
Second solution laplace-plane pole right ascension: 77.3 deg
Second solution laplace-plane pole declination: 15.2 deg
Second solution laplace-plane tilt: 180.0 deg
Second solution mean elements reference: 10

Source and provenance

Original source: ssd.jpl.nasa.gov
Published on Koskamo by: Koskamo
Citation version: Document v1
Reuse: NASA/JPL Solar System Dynamics planetary satellite mean elements and physical parameters (ssd.jpl.nasa.gov/sats), a work of the US government (public domain in the United States)

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Corrected text

Puck is a natural satellite of Uranus in the NASA/JPL Solar System Dynamics planetary satellite tables.

- Planet: Uranus
- Satellite: Puck
- Satellite code: 715
- Physical parameters: not listed in the NASA/JPL planetary satellite physical parameters table
- Ephemeris: URA182
- Reference frame: equatorial
- Epoch (TDB): 2000-01-01.5
- Semi-major axis a: 86004. km
- Eccentricity e: 0.000
- Argument of periapsis ω: 0.0 deg
- Mean anomaly M: 50.1 deg
- Inclination i: 0.3 deg
- Longitude of ascending node: 216.1 deg
- Sidereal period P: 0.761833 days
- Argument of periapsis precession period: 2.226 yr
- Longitude of ascending node precession period: 4.454 yr
- Mean elements reference: 45
- Second solution ephemeris: URA184
- Second solution reference frame: Laplace
- Second solution epoch (TDB): 2025-01-01.0
- Second solution semi-major axis a: 86007. km
- Second solution eccentricity e: 0.009
- Second solution argument of periapsis ω: 337.0 deg
- Second solution mean anomaly M: 264.1 deg
- Second solution inclination i: 1.1 deg
- Second solution longitude of ascending node: 111.2 deg
- Second solution sidereal period P: 0.7618 days
- Second solution argument of periapsis precession period: 1.9 yr
- Second solution longitude of ascending node precession period: 3.9 yr
- Second solution laplace-plane pole right ascension: 77.3 deg
- Second solution laplace-plane pole declination: 15.2 deg
- Second solution laplace-plane tilt: 180.0 deg
- Second solution mean elements reference: 10

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Version history

Published by Koskamo2026-10-05
Version 1